Global Patent Index - EP 1166937 A3

EP 1166937 A3 20040811 - Reparing method of metallic elements

Title (en)

Reparing method of metallic elements

Title (de)

Verfahren zur Instandsetzung von metallischen Bauteilen

Title (fr)

Méthode de réparation d'éléments métalliques

Publication

EP 1166937 A3 20040811 (DE)

Application

EP 01114965 A 20010620

Priority

DE 10030776 A 20000623

Abstract (en)

[origin: EP1166937A2] Process for repairing metallic parts of gas turbines comprises: (a) mechanically radiating the surfaces with a non-oxidic jet material; (b) closing open groove ends by build-up welding a welding material relative to the component material; (c) filling the groove closed on one end side with a solder powder with or without a filler; (d) heating the solder powder in a vacuum until it becomes liquid and metallurgically joins with the component material; and (e) removing the solidified solder. Preferred Features: The jet material is silicon carbide. After the solder has been liquefied and solidified in the groove, it is annealed in a vacuum.

IPC 1-7

B23K 1/00

IPC 8 full level

B23K 1/00 (2006.01); B23K 9/04 (2006.01); B23P 6/00 (2006.01); C23C 24/10 (2006.01); C23C 26/02 (2006.01)

CPC (source: EP US)

B23K 1/0018 (2013.01 - EP US); B23K 9/044 (2013.01 - EP US); B23P 6/007 (2013.01 - EP US); C23C 24/10 (2013.01 - EP US); C23C 26/02 (2013.01 - EP US); B23K 2101/001 (2018.07 - EP US); Y10T 29/4973 (2015.01 - EP US); Y10T 29/49732 (2015.01 - EP US)

Citation (search report)

Designated contracting state (EPC)

AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR

DOCDB simple family (publication)

EP 1166937 A2 20020102; EP 1166937 A3 20040811; EP 1166937 B1 20050831; CA 2351292 A1 20011223; CA 2351292 C 20090901; DE 10030776 A1 20020221; DE 10030776 C2 20020620; DE 50107254 D1 20051006; US 2002020734 A1 20020221; US 6626350 B2 20030930

DOCDB simple family (application)

EP 01114965 A 20010620; CA 2351292 A 20010622; DE 10030776 A 20000623; DE 50107254 T 20010620; US 88754401 A 20010625